EP0384045B1 - Verfahren zur Herstellung einer metallurgischen Verbindung zwischen einem metallischen Material oder einem Verbundwerkstoff mit einer Metallmatrix und einem Metallguss oder Metall-Legierungsguss - Google Patents

Verfahren zur Herstellung einer metallurgischen Verbindung zwischen einem metallischen Material oder einem Verbundwerkstoff mit einer Metallmatrix und einem Metallguss oder Metall-Legierungsguss Download PDF

Info

Publication number
EP0384045B1
EP0384045B1 EP89202324A EP89202324A EP0384045B1 EP 0384045 B1 EP0384045 B1 EP 0384045B1 EP 89202324 A EP89202324 A EP 89202324A EP 89202324 A EP89202324 A EP 89202324A EP 0384045 B1 EP0384045 B1 EP 0384045B1
Authority
EP
European Patent Office
Prior art keywords
metal
casting
process according
composite material
reinforcing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP89202324A
Other languages
English (en)
French (fr)
Other versions
EP0384045A2 (de
EP0384045A3 (en
Inventor
Steven Antony Gedeon
Renato Guerriero
Ilario Tangerini
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Temav SpA
Original Assignee
Temav SpA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Temav SpA filed Critical Temav SpA
Priority to AT89202324T priority Critical patent/ATE93754T1/de
Publication of EP0384045A2 publication Critical patent/EP0384045A2/de
Publication of EP0384045A3 publication Critical patent/EP0384045A3/en
Application granted granted Critical
Publication of EP0384045B1 publication Critical patent/EP0384045B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00Casting in, on, or around objects which form part of the product
    • B22D19/14Casting in, on, or around objects which form part of the product the objects being filamentary or particulate in form
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00Casting in, on, or around objects which form part of the product
    • B22D19/0081Casting in, on, or around objects which form part of the product pretreatment of the insert, e.g. for enhancing the bonding between insert and surrounding cast metal

Definitions

  • the present invention relates to a process for obtaining a metallurgical bond between a metal material, or a composite material having a metal matrix, and a metal casting piece, or a metal-alloy casting according to the preamble of claim 1.
  • a process for obtaining a metallurgical bond between a metal material, or a composite material having a metal matrix, and a metal casting piece, or a metal-alloy casting according to the preamble of claim 1.
  • such a process makes it possible predetermined regions of stationary, or moving, mechanical components to be reinforced by means of the introduction of inserts, or makes it also possible two or more cast pieces to be coupled with one another.
  • the present Applicant has found now that by means of a suitable surface treatment of the material (either a reinforcing material or a material to be coupled), a strong metallurgical bond can be obtained between the same material and the casting.
  • the process according to the present invention which could be given the name of "welding by casting” or “cast-welding”, guarantees that all of the classic requirements of the welding operations are met: namely, the removal of the surface impurities and oxides, intimate contact and coalescence of the materials to be mutually bonded.
  • metals not easily coupled by means of other techniques can be bonded to each other by means of such a type of welding.
  • the process according to the present invention for obtaining a metallurgical bond between a metal material, or a composite material having a metal matrix, and a metal casting, or a metal-alloy casting is characterized by the features as laid out in the characterizing portion of claim 1.
  • the metal material which can be constituted by a single metal or by a metal alloy, or the metal-matrix composite can be, e.g., an insert for reinforcing predetermied regions of either stationary or moving mechanical components subject to wear, (such as guides, pistons, gearwheels, and so forth), or a cast piece to be coupled with one or more cast piece(s) on order to possibly constitute a complex shaped piece, which otherways cannot be obtained, or which can be difficultly obtained (owing to hindrances due to the geometry of the piece or to the type of material, or to a too high cost).
  • the metal composite material and the cast material can have different compositions, and the therein contained metals can be preferably selected from the group consisting of Al, Zn, Pb, Mg, Cu, Sn, In, Ag, Au, It and their alloys.
  • the material can also be a composite having a metal matrix: such a type of material is constituted by a metal phase (or by a metal-alloy phase), which surrounds and bonds other phases, which constitute the reinforcement (powders or ceramic fibres).
  • the reinforcement is endowed with high values of mechanical strength and hardness, and to it the stresses are transferred, which the matrix is submitted to; the matrix, in its turn, should display suitable characteristics as a function of the forecast application type.
  • the reinforcement can be constituted by long or short ceramic fibres (Al2O3, SiC, C, BN, SiO2, glass), or by ceramic "whiskers” (SiC, Si3N4, B4C, Al2O3), or by non-metal powders (SiC, BN, Si3N4, B4C, SiO2, Al2O3, glass, graphite), or by metal fibres (Be, W, SiC-coated W, B4C-coated W, steel).
  • the methods for preparing the composited can be the following:
  • the composite material can be obtained either directly, or by means of a subsequent mechanical machining.
  • the metal which constitutes the thin layer to be deposited in a thickness preferably comprised within the range of from 10 to 200 nm on the surface of the metal material or the metal-matrix composite material, which thin-layer metal may be different from the metals contained in the material and in the casting, can be preferably selected from the group consisting of Au, Ag, Cu, Ni, Pt, Pd, Cr, W, Ir, Mo, Ta, Nb, Os, Re, Rh, Ru and Zr.
  • the deposition of said thin layer can be preferably carried out by sputtering, or by means of an electrochemical deposition process.
  • the liquid to be submitted to the casting process will be capable of wetting the metal, or metal-matrix composite, material, to a high enough exent in order to transfer heat to it, to wash away the oxide layer existing on the surface of said material and to form a direct bond with the material, in case of a metal material, or with the metal matrix, in case of a composite material.
  • the operating parameters of the casting step have to be so adjusted, as to secure that a proper stream of overheated liquid laps the surfaces of the material.
  • the position of the material be suitably selected and that the shape of the downwards ducts (feed ducts) and of the upwards ducts (outflow) inside the mould be so studied as to oblige the liquid metal to lap, wet and wash the walls of the material before becoming too cold.
  • the metal materials can be obtained by means of techniques known from the prior art (e.g.: gravity casting, pressure casting, or “squeeze casting"), either, directly or with a subsequent processing step.
  • Example 4 was carried out in the same way as Example 1, with the following exceptions:
  • Example 5 was carried out in the same way as Example 2, with the following exceptions:
  • Example 6 was carried out in the same way as Example 3, with the following exceptions:

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Laminated Bodies (AREA)
  • Mold Materials And Core Materials (AREA)

Claims (10)

  1. Verfahren zur Ausbildung einer metallurgischen Bindung zwischen:
    (a) einem Metallmaterial oder einem eine Metallmatrix aufweisenden Verbundmaterial, welches Verbundmaterial durch ein Verstärkungsmaterial, ausgewählt unter langen und kurzen keramischen Fasern, keramischen Whiskern, nicht-metallischen Pulvern und Metallfasern, verstärkt ist, und
    (b) einem Metall- oder Metallegierungsguß,
    worin die Metalle von (a) und (b) unter Al, Zn, Pb, Mg, Cu, Sn, In, Ag, Au, Ti und Legierungen hievon ausgewählt sind, welches Verfahren die Stufen einer Durchfuhrung einer Oberflächenbehandlung auf (a) durch Abscheiden einer dünnen Schicht aus einem Metall hierauf, welches Metall ein anderes ist als irgendeines der in (a) und (b) enthaltenen Metalle, des Anordnens von (a) in einer Form und des Gießens des Metalls oder der Metallegierung (b) um (a) umfaßt,
    dadurch gekennzeichnet, daß das Metall, das von den in (a) und (b) enthaltenen verschieden ist, unter Au, Ag, Ni, Pt, Pd, Cr, W, Ir, Mo, Ta, Nb, Os, Re, Rh und Zr ausgewählt ist, wobei die Abscheidung der genannten dünnen Schicht nach einer der folgenden Methoden erfolgt:
    - Sputtern;
    - Plasmaspritzen;
    - Laser-assistierte Abscheidung;
    - Thermo-Verdampfungsabscheidung;
    - Magnetron-assistierte Abscheidung und
    - Gasphasenabscheidung (CVD).
  2. Verfahren nach Anspruch 1, worin die keramischen Verstärkungsfasern für das Verbundmaterial (a) unter keramischen Fasern aus Al₂O₃, Sic, BN, SiO₂ und Glas ausgewählt sind.
  3. Verfahren nach Anspruch 1, worin die Verstärkungswhisker für das Verbundmaterial (a) unter Whiskern aus SiC, Si₃N₄, B₄C und Al₂O₃ ausgewählt sind.
  4. Verfahren nach Anspruch 1, worin die nicht-metallischen Verstärkungspulver für das Verbundmaterial (a) unter pulverförmigem SiC, BN, B₄C, Si₃N₄, SiO₂, Al₂O₃, Glas und Graphit ausgewählt sind.
  5. Verfahren nach Anspruch 1, worin die metallischen Verstärkungsfasern für das Verbundmaterial (a) unter Metallfasern aus Be, W, SiC-beschichtetem w, B₄C-beschichtetem w oder Stahl ausgewählt sind.
  6. Verfahren nach Anspruch 1, worin das Material (a) durch Schwerkraftgießen, Druckgießen oder Preßgießen hergestellt wird.
  7. Verfahren nach Anspruch 1, worin das Material (b) durch Schwerkraftgießen, Druckgießen oder Preßgießen hergestellt wird.
  8. Verfahren nach Anspruch 1, worin -das eine Metallmatrix aufweisende Verbundmaterial (b) durch Dispergieren des Verstärkungsmaterials in der Matrix im geschmolzenen oder im teilweise festen Zustand oder durch Pulvermetallurgie, Fasermetallisierung oder Schichtkompaktieren oder durch Infiltration hergestellt wird.
  9. Verfahren nach Anspruch 8, welches weiterhin eine Bearbeitungsstufe des erhaltenen Materials umfaßt.
  10. Verfahren nach Anspruch 1, worin die abgelagerte dünne Metallschicht eine Stärke von 10 nm bis 200 nm aufweist.
EP89202324A 1989-02-22 1989-09-15 Verfahren zur Herstellung einer metallurgischen Verbindung zwischen einem metallischen Material oder einem Verbundwerkstoff mit einer Metallmatrix und einem Metallguss oder Metall-Legierungsguss Expired - Lifetime EP0384045B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AT89202324T ATE93754T1 (de) 1989-02-22 1989-09-15 Verfahren zur herstellung einer metallurgischen verbindung zwischen einem metallischen material oder einem verbundwerkstoff mit einer metallmatrix und einem metallguss oder metalllegierungsguss.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IT8919516A IT1228449B (it) 1989-02-22 1989-02-22 Procedimento per ottenere un legame metallurgico tra un materiale metallico o composito a matrice metallica e un getto di metallo o di lega metallica.
IT1951689 1989-02-22

Publications (3)

Publication Number Publication Date
EP0384045A2 EP0384045A2 (de) 1990-08-29
EP0384045A3 EP0384045A3 (en) 1990-12-19
EP0384045B1 true EP0384045B1 (de) 1993-09-01

Family

ID=11158693

Family Applications (1)

Application Number Title Priority Date Filing Date
EP89202324A Expired - Lifetime EP0384045B1 (de) 1989-02-22 1989-09-15 Verfahren zur Herstellung einer metallurgischen Verbindung zwischen einem metallischen Material oder einem Verbundwerkstoff mit einer Metallmatrix und einem Metallguss oder Metall-Legierungsguss

Country Status (10)

Country Link
US (1) US4980123A (de)
EP (1) EP0384045B1 (de)
JP (1) JPH02220759A (de)
CN (1) CN1045049A (de)
AT (1) ATE93754T1 (de)
BR (1) BR8905576A (de)
CA (1) CA1325706C (de)
DE (1) DE68908870T2 (de)
ES (1) ES2042977T3 (de)
IT (1) IT1228449B (de)

Families Citing this family (38)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2663250A1 (fr) * 1990-06-19 1991-12-20 Peugeot Procede de fabrication de pieces en alliage d'aluminium coule comportant un insert et culasse de moteur a combustion interne obtenue par ce procede.
FR2665383A1 (fr) * 1990-07-31 1992-02-07 Pechiney Recherche Procede d'obtention par moulage de pieces bimateriaux.
CH682307A5 (de) * 1991-02-05 1993-08-31 Alusuisse Lonza Services Ag
US5295528A (en) * 1991-05-17 1994-03-22 The United States Of America As Represented By The Secretary Of The Navy Centrifugal casting of reinforced articles
US5337803A (en) * 1991-05-17 1994-08-16 The United States Of America As Represented By The Secretary Of The Navy Method of centrifugally casting reinforced composite articles
US5100049A (en) * 1991-07-01 1992-03-31 The United States Of America As Represented By The Secretary Of The Navy Method of bonding carbon-carbon and metal matrix composite structures
FR2688154A1 (fr) * 1992-03-04 1993-09-10 Pechiney Recherche Procede d'obtention de pieces bimateriaux par surmoulage d'un insert revetu d'un film metallique.
US5165592A (en) * 1992-03-31 1992-11-24 J & L Plate, Inc. Method of making refiner plate bars
US5273708A (en) * 1992-06-23 1993-12-28 Howmet Corporation Method of making a dual alloy article
US5433511A (en) * 1993-10-07 1995-07-18 Hayes Wheels International, Inc. Cast wheel reinforced with a metal matrix composite
US5455118A (en) * 1994-02-01 1995-10-03 Pcc Composites, Inc. Plating for metal matrix composites
WO1996018753A1 (en) * 1994-12-15 1996-06-20 Hayes Wheels International, Inc. Thermal deposition methods for enhancement of vehicle wheels
US5526977A (en) * 1994-12-15 1996-06-18 Hayes Wheels International, Inc. Method for fabricating a bimetal vehicle wheel
AT409599B (de) * 1999-04-19 2002-09-25 Boehler Ybbstal Band Gmbh & Co Verbundkörper
US6484790B1 (en) * 1999-08-31 2002-11-26 Cummins Inc. Metallurgical bonding of coated inserts within metal castings
US6443211B1 (en) * 1999-08-31 2002-09-03 Cummins Inc. Mettallurgical bonding of inserts having multi-layered coatings within metal castings
FR2803783B1 (fr) * 2000-01-13 2002-04-26 Valfond Argentan S A Piece bimetallique en alliage d'aluminium comportant un insert massif en titane ou alliage de titane
US6502774B1 (en) 2000-03-08 2003-01-07 J + L Fiber Services, Inc. Refiner disk sensor and sensor refiner disk
US6778936B2 (en) 2000-03-08 2004-08-17 J & L Fiber Services, Inc. Consistency determining method and system
US6752165B2 (en) 2000-03-08 2004-06-22 J & L Fiber Services, Inc. Refiner control method and system
CN1108211C (zh) * 2000-09-14 2003-05-14 四川大学 铁基表面复合材料凸轮轴及其制造方法
US6938843B2 (en) 2001-03-06 2005-09-06 J & L Fiber Services, Inc. Refiner control method and system
JP2003053508A (ja) * 2001-08-14 2003-02-26 Nissan Motor Co Ltd 熱伝導円筒部材およびその製造方法ならびに熱伝導円筒部材を用いたアルミニウム合金製エンジン
FR2831845B1 (fr) * 2001-11-07 2004-05-21 Peugeot Citroen Automobiles Sa Procede et dispositif de coulee d'une piece metallique comportant un element de renforcement
JP2003268511A (ja) * 2002-03-18 2003-09-25 Fuji Heavy Ind Ltd 金属基複合材形成用プリフォーム及びその製造方法、並びにプリフォームを有するジャーナル構造
AU2003251789A1 (en) * 2002-08-20 2004-03-11 3M Innovative Properties Company Metal matrix composites, and methods for making the same
US7104480B2 (en) 2004-03-23 2006-09-12 J&L Fiber Services, Inc. Refiner sensor and coupling arrangement
DE102004029070B4 (de) * 2004-06-16 2009-03-12 Daimler Ag Verfahren zum Eingießen eines Rohlings aus Eisenlegierung in ein Aluminium-Gussteil
US20060024490A1 (en) * 2004-07-29 2006-02-02 3M Innovative Properties Company Metal matrix composites, and methods for making the same
US20060021729A1 (en) * 2004-07-29 2006-02-02 3M Innovative Properties Company Metal matrix composites, and methods for making the same
US20060239825A1 (en) * 2005-04-21 2006-10-26 Honeywell International Inc. Bi-cast blade ring for multi-alloy turbine rotor
US8283047B2 (en) 2006-06-08 2012-10-09 Howmet Corporation Method of making composite casting and composite casting
US7588179B2 (en) * 2007-03-30 2009-09-15 Honeywell International Inc. Bonding of carbon fibers to metal inserts for use in composites
CN101899631B (zh) * 2010-07-26 2012-10-03 辽宁石油化工大学 一种金属基复合材料增强体表面高润湿性涂层改性方法
KR20130074030A (ko) * 2011-12-26 2013-07-04 두산인프라코어 주식회사 열변위 저감을 위한 공작기계용 베이스 구조물 제조방법 및 그 방법에 의해 제조된 베이스 구조물
CN103639395B (zh) * 2013-12-25 2015-12-02 马鞍山市博友神斧刃模具厂 一种镶钢刃具冶金结合的生产方法
CN108672685A (zh) * 2018-05-21 2018-10-19 邱洪 陶瓷管与金属直接铸造的三层复合管
CN110465643B (zh) * 2019-09-12 2021-02-26 江西省鹰潭铜产业工程技术研究中心 一种铜铌复合材料的制备方法

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3841386A (en) * 1971-04-01 1974-10-15 I Niimi Method of joining a beryllium workpiece to light metals
US3920360A (en) * 1974-05-30 1975-11-18 Gen Motors Corp Aluminum-iron composite rotor housing for a rotary combustion engine and method of making the same
DE3005082A1 (de) * 1980-02-12 1981-08-20 Karl Schmidt Gmbh, 7107 Neckarsulm Leichtmetallkolben
US4710235A (en) * 1984-03-05 1987-12-01 Dresser Industries, Inc. Process for preparation of liquid phase bonded amorphous materials
JPS60223654A (ja) * 1984-04-20 1985-11-08 Mazda Motor Corp 異種金属の鋳ぐるみ方法
FR2608476B1 (fr) * 1986-12-18 1989-05-12 Peugeot Procede de fabrication de pieces metalliques coulees comportant un insert en matiere ceramique
DE3723650A1 (de) * 1987-07-17 1989-01-26 Krupp Gmbh Verfahren zur beschichtung von prothesen aus titan und titanlegierungen

Also Published As

Publication number Publication date
JPH02220759A (ja) 1990-09-03
EP0384045A2 (de) 1990-08-29
IT1228449B (it) 1991-06-19
CN1045049A (zh) 1990-09-05
CA1325706C (en) 1994-01-04
EP0384045A3 (en) 1990-12-19
ATE93754T1 (de) 1993-09-15
ES2042977T3 (es) 1993-12-16
DE68908870T2 (de) 1994-02-03
IT8919516A0 (it) 1989-02-22
BR8905576A (pt) 1991-04-30
US4980123A (en) 1990-12-25
DE68908870D1 (de) 1993-10-07

Similar Documents

Publication Publication Date Title
EP0384045B1 (de) Verfahren zur Herstellung einer metallurgischen Verbindung zwischen einem metallischen Material oder einem Verbundwerkstoff mit einer Metallmatrix und einem Metallguss oder Metall-Legierungsguss
Huda et al. MMCs: materials, manufacturing and mechanical properties
McKimpson et al. Processing and properties of metal matrix composites containing discontinuous reinforcement
Ward-Close et al. A fibre coating process for advanced metal-matrix composites
Singh et al. An overview of metal matrix composite: processing and SiC based mechanical properties
US5130209A (en) Arc sprayed continuously reinforced aluminum base composites and method
Singer Metal matrix composites made by spray forming
EP0532434B1 (de) Verfahren zur Herstellung von Verbundgussstücken und so hergestellte Gussstücke
CA3108090C (en) Process and composition for formation of hybrid aluminum composite coating
Huda et al. Metal-matrix composites: Manufacturing aspects. Part I
EP0511318A1 (de) Plasmasprühen von schnell erstarrten aluminiumbasislegierungen.
EP0765946A1 (de) Verfahren zur Herstellung von Verbundmaterial auf Magnesiumbasis
CN1048537A (zh) 金属陶瓷复合材料的生产方法
Durrant et al. Squeeze cast aluminium reinforced with mild steel inserts
Yang et al. Casting particulate and fibrous metal-matrix composites by vacuum infiltration of a liquid metal under an inert gas pressure
Hynes et al. Production of aluminium metal matrix composites by liquid processing methods
EP0370546B1 (de) Verfahren zur Herstellung von Verbundmaterial mit einer Metallmatrix mit kontrollierter Verstärkungsphase
EP0450722A1 (de) Verfahren fÀ¼r einen kontinuierlichen Metallbund zwischen Zylinderfutter und Kurbelgehäuseguss einer Brennkraftmaschine
JPH0798263B2 (ja) 金属薄膜で被覆した挿入物をもつ板を鋳造することにより得られる複合材料部材の製造方法
EP0499628A1 (de) Kontinuierlich verstärkte verbundwerkstoffe auf aluminiumbasis, hergestellt durch plasmaspritzen
JP2909546B2 (ja) 金属基複合材料の製造方法
US5249620A (en) Process for producing composite materials with a metal matrix with a controlled content of reinforcer agent
JP3245338B2 (ja) 低アルミニウム亜鉛基合金用ホットチャンバーダイカストマシン
EP0513238B1 (de) Bogenspritzen von rasch abgekühlten aluminiumlegierungen
JPH0636983B2 (ja) 部分的複合部材の製造方法

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AT BE CH DE ES FR GB GR LI LU NL SE

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AT BE CH DE ES FR GB GR LI LU NL SE

17P Request for examination filed

Effective date: 19910330

17Q First examination report despatched

Effective date: 19920409

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE CH DE ES FR GB GR LI LU NL SE

REF Corresponds to:

Ref document number: 93754

Country of ref document: AT

Date of ref document: 19930915

Kind code of ref document: T

REF Corresponds to:

Ref document number: 68908870

Country of ref document: DE

Date of ref document: 19931007

ET Fr: translation filed
EPTA Lu: last paid annual fee
REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2042977

Country of ref document: ES

Kind code of ref document: T3

REG Reference to a national code

Ref country code: GR

Ref legal event code: FG4A

Free format text: 3009478

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: LU

Payment date: 19940901

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 19940906

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: ES

Payment date: 19940907

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: AT

Payment date: 19940912

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: BE

Payment date: 19940914

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GR

Payment date: 19940928

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 19940930

Year of fee payment: 6

Ref country code: NL

Payment date: 19940930

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CH

Payment date: 19941227

Year of fee payment: 6

EAL Se: european patent in force in sweden

Ref document number: 89202324.3

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 19950915

Ref country code: GB

Effective date: 19950915

Ref country code: AT

Effective date: 19950915

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Effective date: 19950916

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 19950916

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Effective date: 19950930

Ref country code: CH

Effective date: 19950930

Ref country code: BE

Effective date: 19950930

BERE Be: lapsed

Owner name: TEMAV S.P.A.

Effective date: 19950930

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GR

Free format text: THE PATENT HAS BEEN ANNULLED BY A DECISION OF A NATIONAL AUTHORITY

Effective date: 19960331

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Effective date: 19960401

REG Reference to a national code

Ref country code: FR

Ref legal event code: TP

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 19950915

REG Reference to a national code

Ref country code: FR

Ref legal event code: TP

Ref country code: CH

Ref legal event code: PL

REG Reference to a national code

Ref country code: GR

Ref legal event code: MM2A

Free format text: 3009478

NLV4 Nl: lapsed or anulled due to non-payment of the annual fee

Effective date: 19960401

EUG Se: european patent has lapsed

Ref document number: 89202324.3

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 19980729

Year of fee payment: 10

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 19981026

Year of fee payment: 10

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20000531

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20000701

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 19961011